ardupilot

Commit Graph

Author	SHA1	Message	Date
Peter Barker	1f5165349e	Plane: correct compilation when airspeed disabled	3 years ago
Peter Barker	6b48a8df02	Tools: correct antennatracker name in size_compare_branches.py	3 years ago
Andrew Tridgell	62db423758	Tools: update MatekL431 bootloaders	3 years ago
Andrew Tridgell	54e4c6e1be	hwdef: leave MatekL431 ROMFS uncompressed this allows for bl update when low on memory	3 years ago
mateksys	b3f7556ac2	Tools: add MatekL431 bootloader	3 years ago
mateksys	35ed87a5db	AP_HAL_ChibiOS: add MatekL431 AP_Periph hwdef	3 years ago
Andrew Tridgell	994e1e0c0a	AP_Periph: mark version as 1.4.0dev	3 years ago
Andrew Tridgell	59456b4f82	AP_Periph: updated release notes for 1.3.0	3 years ago
Andrew Tridgell	116c692e2b	AP_Periph: rename ReleaseNotes.txt be consistent with plane and copter	3 years ago
Andrew Tridgell	2c22cbc50e	Plane: update release notes for 4.2.0beta3	3 years ago
Henry Wurzburg	14700063d2	ArduPlane: convert floating point divides into multiplys	3 years ago
Henry Wurzburg	c48b7319bc	AP_RSSI: convert floating point divides into multiplys	3 years ago
Andrew Tridgell	6ebefbdb16	Plane: added airspeed based pitch limit check prevent using too much pitch when at low airspeed, which can lead to severe instability in SLT quadplanes	3 years ago
Andrew Tridgell	eabdaae1e7	Plane: use set_lean_angle_max_cd() allows for a wider range of Q_TRANS_DECEL while landing on the desired landing point	3 years ago
Andrew Tridgell	7bb129aa3e	AC_AttitudeControl: added set_lean_angle_max_cd()	3 years ago
Andrew Tridgell	7dcdeac7ab	AC_Autorotation: use accel_to_angle()	3 years ago
Andrew Tridgell	f824be726c	AC_WPNav: use angle/accel functions	3 years ago
Andrew Tridgell	ca4151be2c	AP_Math: added angle_to_accel() and accel_to_angle()	3 years ago
Andrew Tridgell	cc6fc2b130	Plane: improvements to POSITION1 controller this improves 4 things in the POSITION1 controller based on logs from 4.2.0beta2. The changes are designed to increase the tolerance to an incorrect value for Q_TRANS_DECEL, reducing landing overshoot 1) we fix the initialisation of the acceleration. The init_xy_controller() function assumes zero accel, so we need to call set_accel_desired_xy_cmss() just after that init to get the correct accel. Thanks to Leonard for this fix 2) if we decel more than expected due to too low Q_TRANS_DECEL we need to reduce the target speed, rather than putting the nose down 3) lower the default Q_P_JERK_XY to a value more appropriate for most quadplanes (Leonard suggested a value of 2) 4) fixed the pitch envelope from Q_BACKTRANS_MS to start after the airbrake phase is complete	3 years ago
Andrew Tridgell	3772029450	Plane: fixed pitch envelope after AIRBRAKE we need to setup last_fw_mode_ms and last_fw_nav_pitch_cd when we enter POSITION1 mode so that the expanding envelope pitch limit from Q_BACKTRANS_MS is applied correctly	3 years ago
Andrew Tridgell	8b16b5ca94	Plane: adjust throttle mix for auto landing use mix-max during landing approach and initial descent, use min in land final. As discussed with Leonard	3 years ago
Andrew Tridgell	8e64d1cbd7	pymavlink: update submodule	3 years ago
Peter Barker	ebe2205ba7	SITL: add on-hardware example files	3 years ago
Peter Barker	fa2e841387	AP_HAL: honour HAL_SIM_GPS_ENABLED	3 years ago
Peter Barker	e0561b0ca1	GCS_MAVLink: split AP_HAL_SITL and HAL_SIM_ENABLED	3 years ago
Peter Barker	7ad9609fb7	AP_AHRS: split AP_HAL_SITL and HAL_SIM_ENABLED	3 years ago
Peter Barker	318678ac96	Rover: split AP_HAL_SITL and HAL_SIM_ENABLED	3 years ago
Peter Barker	a501a86c8d	Blimp: split AP_HAL_SITL and HAL_SIM_ENABLED	3 years ago
Peter Barker	07b299997d	ArduSub: split AP_HAL_SITL and HAL_SIM_ENABLED	3 years ago
Peter Barker	d93449ac28	ArduPlane: split AP_HAL_SITL and HAL_SIM_ENABLED	3 years ago
Peter Barker	cfd9bfd541	AntennaTracker: split AP_HAL_SITL and HAL_SIM_ENABLED	3 years ago
Peter Barker	df6efc37ac	ArduCopter: split AP_HAL_SITL and AP_SIM_ENABLED	3 years ago
Peter Barker	0bcda3c57e	AP_Vehicle: split AP_HAL_SITL and AP_SIM_ENABLED	3 years ago
Peter Barker	57f8b7c2a8	AP_Compass: split AP_HAL_SITL and AP_SIM_ENABLED	3 years ago
Peter Barker	daedebce2e	AP_Baro: create and use HAL_SIM_BARO_ENABLED	3 years ago
Peter Barker	a53af5277c	AP_InertialSensor: assume accel cals are stored for sitl-on-hw Same as for SITL - they don't need to actually be in storage to be valid	3 years ago
Peter Barker	da21b48f7e	AP_InertialSensor: split AP_HAL_SITL and HAL_SIM_ENABLED	3 years ago
Peter Barker	a402dce95b	AP_HAL: permit double-maths whe simulating	3 years ago
Peter Barker	650ef59be8	AP_HAL: create HAL::SIMState object to hold simulation state	3 years ago
Peter Barker	f7608c22da	AP_HAL_ChibiOS: set pwm output values in simstate object	3 years ago
Peter Barker	8b2f85756a	AP_HAL_ChibiOS: instantiate SIMState object in HAL	3 years ago
Peter Barker	26d6c2413b	AP_Scheduler: update simulation state on embedded	3 years ago
Peter Barker	e07ddf95b4	AP_Math: provide rand_float on embedded hardware	3 years ago
Peter Barker	a9aa5c2d60	AP_GPS: add a new AP_GPS_SITL object	3 years ago
Peter Barker	edef2ceb56	SITL: usleep only on AP_HAL_SITL	3 years ago
Peter Barker	b360521d0b	SITL: permit double-precision maths in SITL even on embedded hardware	3 years ago
Peter Barker	4c8fc3bcaf	waf: split AP_HAL_SITL and AP_SIM_ENABLED	3 years ago
Peter Barker	2e809282e7	SITL: split AP_HAL_SITL and AP_SIM_ENABLED	3 years ago
Peter Barker	0957131543	SITL: use AP_HAL::micros() for get_wall_time_us	3 years ago
Peter Barker	3cf7091525	SITL: make parsing of json files dependent on PICOJSON picojson uses the standard library; this will be a problem on embedded platforms	3 years ago

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52441 Commits (1f5165349efdf6884a657d04c7a0fcaa193070c3) All Branches Search

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